Appendix III - 6A-Series Sections

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Only a few of these 6A sections were published in the book. I have added those that I know were used on a production airplane.
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63A-series cambered airfoils
63A112 63A210 63A412 63A415
63A418 63A421 63A615

64A-series cambered airfoils
64A204 64A106 64A210 64A410
64A212 64A412 64A612 64A114
64A215 64A415 64A218 64A221

65A-series cambered airfoils
65A112 65A210 65A212 65A412
65A215 65A415 65A615
65A418 65A421

NACA Section 63A210
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	0.9451	0.5000	-0.7110
0.7500	1.1275	0.7500	-0.8651
1.2500	1.4294	1.2500	-1.0940
2.5000	1.9954	2.5000	-1.4973
5.0000	2.8123	5.0000	-2.0314
7.5000	3.4367	7.5000	-2.4150
10.0000	3.9480	10.0000	-2.7154
15.0000	4.7502	15.0000	-3.1613
20.0000	5.3430	20.0000	-3.4650
25.0000	5.7740	25.0000	-3.6607
30.0000	6.0670	30.0000	-3.7652
35.0000	6.2210	35.0000	-3.7725
40.0000	6.2466	40.0000	-3.6904
45.0000	6.1489	45.0000	-3.5223
50.0000	5.9407	50.0000	-3.2812
55.0000	5.6343	55.0000	-2.9804
60.0000	5.2410	60.0000	-2.6334
65.0000	4.7696	65.0000	-2.2527
70.0000	4.2284	70.0000	-1.8530
75.0000	3.6293	75.0000	-1.4567
80.0000	2.9821	80.0000	-1.0979
85.0000	2.2649	85.0000	-0.8076
90.0000	1.5269	90.0000	-0.5358
95.0000	0.7718	95.0000	-0.2761
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 0.724 percent c
slope of mean line at LE = 0.0951

NACA 63A210
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.4220	0.8770	0.5780	-0.7646
0.6630	1.0677	0.8370	-0.9096
1.1509	1.3744	1.3491	-1.1332
2.3838	1.9496	2.6162	-1.5277
4.8689	2.7754	5.1311	-2.0542
7.3635	3.4059	7.6365	-2.4333
9.8628	3.9222	10.1372	-2.7301
14.8692	4.7322	15.1308	-3.1708
19.8816	5.3310	20.1184	-3.4708
24.8975	5.7665	25.1025	-3.6637
29.9155	6.0632	30.0845	-3.7661
34.9351	6.2198	35.0649	-3.7720
39.9552	6.2470	40.0448	-3.6892
44.9752	6.1496	45.0248	-3.5212
49.9944	5.9409	50.0056	-3.2808
55.0121	5.6334	54.9879	-2.9811
60.0279	5.2386	59.9722	-2.6354
65.0413	4.7654	64.9587	-2.2560
70.0523	4.2224	69.9477	-1.8572
75.0613	3.6217	74.9387	-1.4614
80.0735	2.9720	79.9265	-1.1027
85.0718	2.2544	84.9282	-0.8116
90.0505	1.5193	89.9495	-0.5385
95.0256	0.7678	94.9744	-0.2774
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 0.724 percent c
slope of mean line at LE = 0.0951

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NACA Section 63A112
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	1.0440	0.5000	-0.9027
0.7500	1.2503	0.7500	-1.0971
1.2500	1.5871	1.2500	-1.3990
2.5000	2.2124	2.5000	-1.9463
5.0000	3.0987	5.0000	-2.6948
7.5000	3.7669	7.5000	-3.2451
10.0000	4.3088	10.0000	-3.6834
15.0000	5.1494	15.0000	-4.3487
20.0000	5.7607	20.0000	-4.8177
25.0000	6.1955	25.0000	-5.1365
30.0000	6.4794	30.0000	-5.3275
35.0000	6.6094	35.0000	-5.3850
40.0000	6.5977	40.0000	-5.3199
45.0000	6.4498	45.0000	-5.1369
50.0000	6.1831	50.0000	-4.8535
55.0000	5.8126	55.0000	-4.4852
60.0000	5.3528	60.0000	-4.0480
65.0000	4.8163	65.0000	-3.5563
70.0000	4.2162	70.0000	-3.0263
75.0000	3.5703	75.0000	-2.4814
80.0000	2.8985	80.0000	-1.9533
85.0000	2.1917	85.0000	-1.4600
90.0000	1.4732	90.0000	-0.9756
95.0000	0.7485	95.0000	-0.4996
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 0.990 percent c
slope of mean line at LE = 0.0475

NACA 63A112
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.4538	0.9993	0.5462	-0.9431
0.6985	1.2109	0.8015	-1.1318
1.1911	1.5510	1.3089	-1.4304
2.4306	2.1825	2.5694	-1.9716
4.9214	3.0750	5.0786	-2.7143
7.4181	3.7473	7.5819	-3.2609
9.9176	4.2925	10.0824	-3.6964
14.9214	5.1381	15.0786	-4.3574
19.9289	5.7533	20.0711	-4.8232
24.9384	6.1910	25.0616	-5.1396
29.9493	6.4773	30.0507	-5.3287
34.9610	6.6089	35.0390	-5.3850
39.9731	6.5981	40.0269	-5.3193
44.9852	6.4504	45.0148	-5.1362
49.9966	6.1833	50.0033	-4.8533
55.0072	5.8120	54.9928	-4.4858
60.0166	5.3511	59.9834	-4.0495
65.0246	4.8135	64.9754	-3.5588
70.0312	4.2123	69.9688	-3.0297
75.0365	3.5655	74.9635	-2.4853
80.0437	2.8925	79.9563	-1.9578
85.0428	2.1856	84.9572	-1.4642
90.0300	1.4689	89.9700	-0.9784
95.0153	0.7462	94.9847	-0.5010
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 0.990 percent c
slope of mean line at LE = 0.0475

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NACA Section 63A412
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	1.2675	0.5000	-0.7126
0.7500	1.4974	0.7500	-0.8852
1.2500	1.8861	1.2500	-1.1361
2.5000	2.6280	2.5000	-1.5647
5.0000	3.7194	5.0000	-2.1048
7.5000	4.5629	7.5000	-2.4761
10.0000	5.2586	10.0000	-2.7576
15.0000	6.3594	15.0000	-3.1571
20.0000	7.1819	20.0000	-3.4100
25.0000	7.7886	25.0000	-3.5529
30.0000	8.2104	30.0000	-3.6027
35.0000	8.4477	35.0000	-3.5504
40.0000	8.5152	40.0000	-3.4042
45.0000	8.4194	45.0000	-3.1679
50.0000	8.1775	50.0000	-2.8591
55.0000	7.8036	55.0000	-2.4943
60.0000	7.3104	60.0000	-2.0912
65.0000	6.7074	65.0000	-1.6673
70.0000	6.0031	70.0000	-1.2434
75.0000	5.2068	75.0000	-0.8511
80.0000	4.3221	80.0000	-0.5417
85.0000	3.2964	85.0000	-0.3697
90.0000	2.2249	90.0000	-0.2345
95.0000	1.1248	95.0000	-0.1291
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 0.990 percent c
slope of mean line at LE = 0.1902

NACA 63A412
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.3184	1.0676	0.6816	-0.8427
0.5467	1.3129	0.9533	-0.9966
1.0170	1.7148	1.4830	-1.2323
2.2248	2.4818	2.7752	-1.6380
4.6874	3.6000	5.3126	-2.1576
7.1737	4.4625	7.8263	-2.5172
9.6716	5.1738	10.3284	-2.7897
14.6864	6.2995	15.3136	-3.1767
19.7158	7.1413	20.2842	-3.4209
24.7538	7.7632	25.2462	-3.5575
29.7972	8.1969	30.2028	-3.6026
34.8442	8.4429	35.1558	-3.5472
39.8926	8.5155	40.1074	-3.4000
44.9407	8.4214	45.0593	-3.1647
49.9866	8.1784	50.0134	-2.8582
55.0289	7.8011	54.9711	-2.4965
60.0665	7.3031	59.9335	-2.0967
65.0985	6.6945	64.9015	-1.6757
70.1246	5.9843	69.8754	-1.2538
75.1458	5.1824	74.8542	-0.8618
80.1745	4.2886	79.8255	-0.5499
85.1703	3.2602	84.8297	-0.3746
90.1195	2.1990	89.8805	-0.2373
95.0609	1.1113	94.9391	-0.1304
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 0.990 percent c
slope of mean line at LE = 0.1902

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NACA Section 63A415
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	-0.0000	0.0000	0.0000
0.5000	1.5546	0.5000	-0.8458
0.7500	1.8295	0.7500	-1.0664
1.2500	2.2944	1.2500	-1.4006
2.5000	3.1820	2.5000	-1.9940
5.0000	4.4785	5.0000	-2.7650
7.5000	5.4739	7.5000	-3.3057
10.0000	6.2909	10.0000	-3.7225
15.0000	7.5762	15.0000	-4.3282
20.0000	8.5291	20.0000	-4.7278
25.0000	9.2249	25.0000	-4.9722
30.0000	9.6981	30.0000	-5.0833
35.0000	9.9495	35.0000	-5.0519
40.0000	9.9969	40.0000	-4.8889
45.0000	9.8489	45.0000	-4.6007
50.0000	9.5290	50.0000	-4.2116
55.0000	9.0559	55.0000	-3.7438
60.0000	8.4457	60.0000	-3.2192
65.0000	7.7118	65.0000	-2.6598
70.0000	6.8674	70.0000	-2.0920
75.0000	5.9287	75.0000	-1.5545
80.0000	4.9036	80.0000	-1.1013
85.0000	3.7368	85.0000	-0.7883
90.0000	2.5180	90.0000	-0.5128
95.0000	1.2787	95.0000	-0.2752
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 1.406 percent c
slope of mean line at LE = 0.1902

NACA 63A415
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.2804	1.2672	0.7196	-1.0423
0.5035	1.5587	0.9965	-1.2425
0.9653	2.0417	1.5347	-1.5591
2.1602	2.9649	2.8398	-2.1212
4.6111	4.3019	5.3889	-2.8595
7.0929	5.3260	7.9071	-3.3806
9.5898	6.1663	10.4102	-3.7822
14.6077	7.4888	15.3923	-4.3660
19.6443	8.4704	20.3557	-4.7499
24.6918	9.1885	25.3082	-4.9829
29.7462	9.6795	30.2538	-5.0852
34.8052	9.9436	35.1948	-5.0479
39.8659	9.9983	40.1341	-4.8828
44.9260	9.8524	45.0740	-4.5956
49.9833	9.5304	50.0167	-4.2102
55.0359	9.0520	54.9641	-3.7474
60.0825	8.4345	59.9175	-3.2282
65.1220	7.6925	64.8780	-2.6737
70.1541	6.8398	69.8459	-2.1093
75.1801	5.8935	74.8199	-1.5729
80.2155	4.8562	79.7845	-1.1175
85.2102	3.6859	84.7898	-0.8003
90.1472	2.4819	89.8528	-0.5202
95.0755	1.2597	94.9245	-0.2789
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 1.406 percent c
slope of mean line at LE = 0.1902

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NACA Section 63A615
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	-0.0000	0.0000	0.0000
0.5000	1.7574	0.5000	-0.7140
0.7500	2.0498	0.7500	-0.9119
1.2500	2.5448	1.2500	-1.2115
2.5000	3.5050	2.5000	-1.7264
5.0000	4.9306	5.0000	-2.3625
7.5000	6.0370	7.5000	-2.7862
10.0000	6.9517	10.0000	-3.1004
15.0000	8.4026	15.0000	-3.5314
20.0000	9.4900	20.0000	-3.7886
25.0000	10.2956	25.0000	-3.9168
30.0000	10.8566	30.0000	-3.9347
35.0000	11.1768	35.0000	-3.8305
40.0000	11.2754	40.0000	-3.6134
45.0000	11.1614	45.0000	-3.2892
50.0000	10.8584	50.0000	-2.8823
55.0000	10.3840	55.0000	-2.4158
60.0000	9.7529	60.0000	-1.9132
65.0000	8.9764	65.0000	-1.3984
70.0000	8.0644	70.0000	-0.9014
75.0000	7.0273	75.0000	-0.4660
80.0000	5.8636	80.0000	-0.1607
85.0000	4.4858	85.0000	-0.0631
90.0000	3.0282	90.0000	-0.0203
95.0000	1.5345	95.0000	-0.0293
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 1.406 percent c
slope of mean line at LE = 0.2852

NACA 63A615
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.1776	1.2990	0.8224	-0.9617
0.3870	1.6122	1.1130	-1.1379
0.8293	2.1355	1.6707	-1.4117
1.9958	3.1484	3.0042	-1.8828
4.4209	4.6367	5.5791	-2.4731
6.8927	5.7889	8.1073	-2.8709
9.3872	6.7415	10.6128	-3.1653
14.4132	8.2534	15.5868	-3.5692
19.4674	9.3886	20.5326	-3.8079
24.5383	10.2316	25.4617	-3.9231
29.6196	10.8226	30.3804	-3.9312
34.7079	11.1643	35.2921	-3.8208
39.7989	11.2756	40.2011	-3.6024
44.8891	11.1661	45.1109	-3.2809
49.9750	10.8604	50.0250	-2.8801
55.0539	10.3780	54.9461	-2.4211
60.1237	9.7354	59.8763	-1.9259
65.1830	8.9454	64.8170	-1.4172
70.2310	8.0191	69.7690	-0.9233
75.2697	6.9683	74.7303	-0.4873
80.3222	5.7813	79.6778	-0.1732
85.3136	4.3952	84.6864	-0.0668
90.2195	2.9635	89.7805	-0.0209
95.1125	1.5004	94.8875	-0.0291
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 1.406 percent c
slope of mean line at LE = 0.2852

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NACA Section 63A418
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	1.8226	0.5000	-0.9511
0.7500	2.1423	0.7500	-1.2135
1.2500	2.6849	1.2500	-1.6245
2.5000	3.7246	2.5000	-2.3843
5.0000	5.2327	5.0000	-3.3969
7.5000	6.3836	7.5000	-4.1143
10.0000	7.3239	10.0000	-4.6720
15.0000	8.7963	15.0000	-5.4916
20.0000	9.8805	20.0000	-6.0428
25.0000	10.6655	25.0000	-6.3920
30.0000	11.1883	30.0000	-6.5651
35.0000	11.4513	35.0000	-6.5536
40.0000	11.4750	40.0000	-6.3710
45.0000	11.2712	45.0000	-6.0272
50.0000	10.8698	50.0000	-5.5536
55.0000	10.2950	55.0000	-4.9795
60.0000	9.5663	60.0000	-4.3309
65.0000	8.7008	65.0000	-3.6344
70.0000	7.7168	70.0000	-2.9225
75.0000	6.6378	75.0000	-2.2415
80.0000	5.4752	80.0000	-1.6469
85.0000	4.1704	85.0000	-1.1960
90.0000	2.8056	90.0000	-0.7828
95.0000	1.4317	95.0000	-0.4192
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 1.794 percent c
slope of mean line at LE = 0.1902

NACA 63A418
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.2474	1.4409	0.7526	-1.2160
0.4654	1.7753	1.0346	-1.4591
0.9185	2.3380	1.5815	-1.8554
2.0990	3.4230	2.9010	-2.5793
4.5367	4.9877	5.4633	-3.5453
7.0132	6.1788	7.9868	-4.2335
9.5085	7.1519	10.4915	-4.7678
14.5291	8.6762	15.4709	-5.5534
19.5728	9.8003	20.4272	-6.0799
24.6297	10.6164	25.3703	-6.4108
29.6952	11.1640	30.3048	-6.5697
34.7662	11.4444	35.2338	-6.5488
39.8392	11.4778	40.1608	-6.3623
44.9115	11.2766	45.0885	-6.0198
49.9800	10.8717	50.0200	-5.5515
55.0429	10.2894	54.9571	-4.9848
60.0983	9.5506	59.9017	-4.3442
65.1451	8.6738	64.8549	-3.6550
70.1830	7.6788	69.8170	-2.9483
75.2137	6.5901	74.7863	-2.2695
80.2556	5.4120	79.7444	-1.6733
85.2493	4.1029	84.7507	-1.2173
90.1743	2.7579	89.8257	-0.7962
95.0899	1.4067	94.9101	-0.4258
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 1.794 percent c
slope of mean line at LE = 0.1902

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NACA Section 63A421
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	-0.0000	0.0000	0.0000
0.5000	2.0617	0.5000	-1.0312
0.7500	2.4253	0.7500	-1.3283
1.2500	3.0477	1.2500	-1.8059
2.5000	4.2484	2.5000	-2.7295
5.0000	5.9770	5.0000	-3.9951
7.5000	7.2882	7.5000	-4.8978
10.0000	8.3549	10.0000	-5.6026
15.0000	10.0177	15.0000	-6.6450
20.0000	11.2348	20.0000	-7.3534
25.0000	12.1095	25.0000	-7.8111
30.0000	12.6809	30.0000	-8.0479
35.0000	12.9528	35.0000	-8.0555
40.0000	12.9492	40.0000	-7.8503
45.0000	12.6868	45.0000	-7.4479
50.0000	12.2015	50.0000	-6.8869
55.0000	11.5226	55.0000	-6.2030
60.0000	10.6733	60.0000	-5.4274
65.0000	9.6761	65.0000	-4.5928
70.0000	8.5529	70.0000	-3.7367
75.0000	7.3365	75.0000	-2.9148
80.0000	6.0384	80.0000	-2.1803
85.0000	4.5985	85.0000	-1.5943
90.0000	3.0884	90.0000	-1.0457
95.0000	1.5844	95.0000	-0.5615
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 2.126 percent c
slope of mean line at LE = 0.1902

NACA 63A421
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.2199	1.5853	0.7801	-1.3605
0.4332	1.9577	1.0668	-1.6415
0.8776	2.5963	1.6224	-2.1138
2.0421	3.8489	2.9579	-3.0051
4.4645	5.6520	5.5355	-4.2096
6.9348	7.0170	8.0652	-5.0717
9.4280	8.1275	10.5720	-5.7434
14.4508	9.8597	15.5492	-6.7369
19.5012	11.1299	20.4988	-7.4094
24.5676	12.0459	25.4324	-7.8402
29.6441	12.6503	30.3559	-8.0561
34.7271	12.9453	35.2729	-8.0496
39.8126	12.9542	40.1874	-7.8387
44.8969	12.6946	45.1031	-7.4378
49.9768	12.2042	50.0232	-6.8840
55.0497	11.5149	54.9503	-6.2103
60.1139	10.6521	59.8861	-5.4458
65.1679	9.6403	64.8321	-4.6215
70.2114	8.5031	69.7886	-3.7725
75.2467	7.2747	74.7533	-2.9541
80.2949	5.9576	79.7051	-2.2189
85.2877	4.5124	84.7123	-1.6268
90.2008	3.0279	89.7992	-1.0662
95.1042	1.5526	94.8958	-0.5718
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 2.126 percent c
slope of mean line at LE = 0.1902

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NACA Section 64A204
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	0.4052	0.5000	-0.2717
0.7500	0.4925	0.7500	-0.3183
1.2500	0.6350	1.2500	-0.3792
2.5000	0.9042	2.5000	-0.4714
5.0000	1.3029	5.0000	-0.5731
7.5000	1.6156	7.5000	-0.6358
10.0000	1.8798	10.0000	-0.6817
15.0000	2.3062	15.0000	-0.7407
20.0000	2.6363	20.0000	-0.7732
25.0000	2.8900	25.0000	-0.7854
30.0000	3.0785	30.0000	-0.7804
35.0000	3.2074	35.0000	-0.7592
40.0000	3.2775	40.0000	-0.7198
45.0000	3.2794	45.0000	-0.6513
50.0000	3.2180	50.0000	-0.5580
55.0000	3.1015	55.0000	-0.4489
60.0000	2.9353	60.0000	-0.3314
65.0000	2.7223	65.0000	-0.2117
70.0000	2.4630	70.0000	-0.0960
75.0000	2.1579	75.0000	0.0046
80.0000	1.8018	80.0000	0.0702
85.0000	1.3753	85.0000	0.0701
90.0000	0.9310	90.0000	0.0517
95.0000	0.4673	95.0000	0.0241
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 0.123 percent c
slope of mean line at LE = 0.0951

NACA 64A204
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.4681	0.3916	0.5319	-0.2791
0.7146	0.4814	0.7854	-0.3233
1.2102	0.6246	1.2898	-0.3833
2.4543	0.8957	2.5457	-0.4738
4.9492	1.2959	5.0508	-0.5747
7.4475	1.6096	7.5525	-0.6369
9.9473	1.8746	10.0527	-0.6825
14.9496	2.3025	15.0504	-0.7411
19.9542	2.6336	20.0458	-0.7734
24.9601	2.8883	25.0399	-0.7854
29.9668	3.0775	30.0332	-0.7803
34.9742	3.2069	35.0258	-0.7591
39.9820	3.2774	40.0180	-0.7196
44.9899	3.2795	45.0101	-0.6511
49.9977	3.2181	50.0023	-0.5580
55.0050	3.1013	54.9950	-0.4490
60.0116	2.9349	59.9884	-0.3317
65.0173	2.7215	64.9827	-0.2121
70.0220	2.4618	69.9780	-0.0965
75.0260	2.1562	74.9740	0.0041
80.0312	1.7993	79.9688	0.0700
85.0305	1.3726	84.9695	0.0702
90.0215	0.9290	89.9785	0.0518
95.0108	0.4663	94.9892	0.0241
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 0.123 percent c
slope of mean line at LE = 0.0951

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NACA Section 64A106
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	-0.0000	0.0000	0.0000
0.5000	0.5417	0.5000	-0.4625
0.7500	0.6510	0.7500	-0.5537
1.2500	0.8233	1.2500	-0.6865
2.5000	1.1389	2.5000	-0.9155
5.0000	1.5897	5.0000	-1.2194
7.5000	1.9347	7.5000	-1.4403
10.0000	2.2226	10.0000	-1.6198
15.0000	2.6794	15.0000	-1.8939
20.0000	3.0261	20.0000	-2.0928
25.0000	3.2860	25.0000	-2.2326
30.0000	3.4716	30.0000	-2.3220
35.0000	3.5890	35.0000	-2.3646
40.0000	3.6372	40.0000	-2.3584
45.0000	3.6008	45.0000	-2.2869
50.0000	3.4894	50.0000	-2.1595
55.0000	3.3154	55.0000	-1.9890
60.0000	3.0883	60.0000	-1.7859
65.0000	2.8138	65.0000	-1.5577
70.0000	2.4957	70.0000	-1.3111
75.0000	2.1411	75.0000	-1.0585
80.0000	1.7540	80.0000	-0.8164
85.0000	1.3302	85.0000	-0.6059
90.0000	0.8977	90.0000	-0.4052
95.0000	0.4522	95.0000	-0.2059
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 0.277 percent c
slope of mean line at LE = 0.0475

NACA 64A106
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.4762	0.5291	0.5238	-0.4729
0.7235	0.6407	0.7765	-0.5617
1.2202	0.8141	1.2798	-0.6934
2.4657	1.1316	2.5343	-0.9206
4.9619	1.5838	5.0381	-1.2232
7.4606	1.9297	7.5394	-1.4434
9.9604	2.2184	10.0396	-1.6223
14.9622	2.6764	15.0378	-1.8957
19.9656	3.0241	20.0344	-2.0940
24.9700	3.2847	25.0300	-2.2333
29.9751	3.4709	30.0249	-2.3223
34.9807	3.5886	35.0193	-2.3647
39.9865	3.6372	40.0135	-2.3583
44.9925	3.6010	45.0075	-2.2868
49.9983	3.4895	50.0017	-2.1594
55.0037	3.3153	54.9963	-1.9891
60.0086	3.0879	59.9914	-1.7863
65.0129	2.8131	64.9871	-1.5584
70.0164	2.4946	69.9836	-1.3120
75.0193	2.1396	74.9807	-1.0595
80.0232	1.7521	79.9768	-0.8174
85.0227	1.3283	84.9773	-0.6069
90.0160	0.8963	89.9840	-0.4058
95.0081	0.4515	94.9919	-0.2063
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 0.277 percent c
slope of mean line at LE = 0.0475

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NACA Section 64A210
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	-0.0000	0.0000	0.0000
0.5000	0.9339	0.5000	-0.7026
0.7500	1.1132	0.7500	-0.8544
1.2500	1.4035	1.2500	-1.0743
2.5000	1.9434	2.5000	-1.4517
5.0000	2.7218	5.0000	-1.9464
7.5000	3.3193	7.5000	-2.3017
10.0000	3.8186	10.0000	-2.5886
15.0000	4.6112	15.0000	-3.0233
20.0000	5.2138	20.0000	-3.3355
25.0000	5.6653	25.0000	-3.5513
30.0000	5.9884	30.0000	-3.6853
35.0000	6.1926	35.0000	-3.7426
40.0000	6.2733	40.0000	-3.7162
45.0000	6.2054	45.0000	-3.5787
50.0000	6.0119	50.0000	-3.3524
55.0000	5.7125	55.0000	-3.0585
60.0000	5.3237	60.0000	-2.7160
65.0000	4.8542	65.0000	-2.3372
70.0000	4.3111	70.0000	-1.9353
75.0000	3.7066	75.0000	-1.5333
80.0000	3.0449	80.0000	-1.1598
85.0000	2.3124	85.0000	-0.8543
90.0000	1.5590	90.0000	-0.5674
95.0000	0.7880	95.0000	-0.2920
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 0.735 percent c
slope of mean line at LE = 0.0951

NACA 64A210
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.4229	0.8674	0.5771	-0.7549
0.6641	1.0555	0.8359	-0.8974
1.1527	1.3519	1.3473	-1.1106
2.3871	1.9010	2.6129	-1.4791
4.8736	2.6879	5.1264	-1.9667
7.3689	3.2908	7.6311	-2.3181
9.8681	3.7943	10.1319	-2.6022
14.8738	4.5938	15.1262	-3.0324
19.8851	5.2017	20.1149	-3.3415
24.8998	5.6576	25.1002	-3.5548
29.9169	5.9840	30.0831	-3.6868
34.9354	6.1907	35.0646	-3.7429
39.9550	6.2732	40.0450	-3.7155
44.9750	6.2061	45.0250	-3.5777
49.9943	6.0122	50.0057	-3.3521
55.0123	5.7116	54.9877	-3.0593
60.0284	5.3213	59.9716	-2.7181
65.0423	4.8499	64.9577	-2.3405
70.0538	4.3049	69.9462	-1.9397
75.0631	3.6986	74.9369	-1.5383
80.0757	3.0343	79.9243	-1.1649
85.0740	2.3013	84.9260	-0.8585
90.0520	1.5511	89.9480	-0.5703
95.0264	0.7838	94.9736	-0.2934
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 0.735 percent c
slope of mean line at LE = 0.0951

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NACA Section 64A410
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	1.0576	0.5000	-0.6003
0.7500	1.2530	0.7500	-0.7359
1.2500	1.5792	1.2500	-0.9217
2.5000	2.2000	2.5000	-1.2171
5.0000	3.1193	5.0000	-1.5689
7.5000	3.8369	7.5000	-1.8019
10.0000	4.4414	10.0000	-1.9815
15.0000	5.4111	15.0000	-2.2354
20.0000	6.1573	20.0000	-2.4008
25.0000	6.7255	25.0000	-2.4975
30.0000	7.1420	30.0000	-2.5358
35.0000	7.4188	35.0000	-2.5189
40.0000	7.5524	40.0000	-2.4383
45.0000	7.5190	45.0000	-2.2655
50.0000	7.3417	50.0000	-2.0227
55.0000	7.0395	55.0000	-1.7316
60.0000	6.6278	60.0000	-1.4125
65.0000	6.1134	65.0000	-1.0794
70.0000	5.5004	70.0000	-0.7488
75.0000	4.7954	75.0000	-0.4488
80.0000	3.9915	80.0000	-0.2215
85.0000	3.0465	85.0000	-0.1301
90.0000	2.0586	90.0000	-0.0752
95.0000	1.0380	95.0000	-0.0460
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 0.735 percent c
slope of mean line at LE = 0.1902

NACA 64A410
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.3478	0.9129	0.6522	-0.6880
0.5801	1.1235	0.9199	-0.8073
1.0571	1.4612	1.4429	-0.9787
2.2757	2.1008	2.7243	-1.2570
4.7484	3.0383	5.2516	-1.5959
7.2386	3.7680	7.7614	-1.8227
9.7369	4.3822	10.2631	-1.9981
14.7481	5.3683	15.2519	-2.2455
19.7704	6.1272	20.2296	-2.4067
24.7998	6.7058	25.2002	-2.5001
29.8338	7.1304	30.1662	-2.5361
34.8709	7.4133	35.1291	-2.5177
39.9100	7.5515	40.0900	-2.4360
44.9499	7.5201	45.0501	-2.2634
49.9886	7.3423	50.0114	-2.0221
55.0246	7.0377	54.9754	-1.7331
60.0569	6.6225	59.9431	-1.4162
65.0846	6.1038	64.9154	-1.0850
70.1075	5.4862	69.8925	-0.7557
75.1262	4.7765	74.8738	-0.4558
80.1512	3.9649	79.8488	-0.2262
85.1476	3.0176	84.8524	-0.1320
90.1037	2.0378	89.8963	-0.0761
95.0526	1.0271	94.9474	-0.0463
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 0.735 percent c
slope of mean line at LE = 0.1902

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NACA Section 64A212
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	1.1028	0.5000	-0.8253
0.7500	1.3117	0.7500	-1.0109
1.2500	1.6511	1.2500	-1.2845
2.5000	2.2830	2.5000	-1.7603
5.0000	3.1910	5.0000	-2.3916
7.5000	3.8857	7.5000	-2.8480
10.0000	4.4649	10.0000	-3.2179
15.0000	5.3813	15.0000	-3.7815
20.0000	6.0758	20.0000	-4.1895
25.0000	6.5936	25.0000	-4.4746
30.0000	6.9614	30.0000	-4.6556
35.0000	7.1897	35.0000	-4.7388
40.0000	7.2702	40.0000	-4.7136
45.0000	7.1746	45.0000	-4.5486
50.0000	6.9331	50.0000	-4.2738
55.0000	6.5696	55.0000	-3.9149
60.0000	6.1043	60.0000	-3.4946
65.0000	5.5474	65.0000	-3.0271
70.0000	4.9098	70.0000	-2.5294
75.0000	4.2065	75.0000	-2.0278
80.0000	3.4457	80.0000	-1.5541
85.0000	2.6144	85.0000	-1.1498
90.0000	1.7608	90.0000	-0.7647
95.0000	0.8924	95.0000	-0.3941
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 1.021 percent c
slope of mean line at LE = 0.0951

NACA 64A212
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.4091	1.0118	0.5909	-0.8993
0.6486	1.2317	0.8514	-1.0736
1.1347	1.5793	1.3653	-1.3380
2.3655	2.2237	2.6345	-1.8018
4.8489	3.1439	5.1511	-2.4227
7.3429	3.8460	7.6571	-2.8733
9.8419	4.4310	10.1581	-3.2390
14.8486	5.3572	15.1514	-3.7959
19.8620	6.0592	20.1380	-4.1989
24.8797	6.5830	25.1203	-4.4801
29.9002	6.9554	30.0998	-4.6583
34.9225	7.1872	35.0775	-4.7393
39.9460	7.2703	40.0540	-4.7125
44.9700	7.1756	45.0300	-4.5472
49.9932	6.9335	50.0068	-4.2734
55.0147	6.5684	54.9853	-3.9161
60.0340	6.1008	59.9661	-3.4977
65.0505	5.5414	64.9495	-3.0320
70.0640	4.9012	69.9360	-2.5359
75.0751	4.1956	74.9249	-2.0352
80.0900	3.4313	79.9100	-1.5620
85.0880	2.5994	84.9120	-1.1566
90.0618	1.7502	89.9382	-0.7693
95.0315	0.8868	94.9685	-0.3964
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 1.021 percent c
slope of mean line at LE = 0.0951

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NACA Section 64A412
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	1.2506	0.5000	-0.7039
0.7500	1.4744	0.7500	-0.8738
1.2500	1.8473	1.2500	-1.1157
2.5000	2.5570	2.5000	-1.5124
5.0000	3.6023	5.0000	-2.0039
7.5000	4.4150	7.5000	-2.3398
10.0000	5.0976	10.0000	-2.6038
15.0000	6.1883	15.0000	-2.9889
20.0000	7.0242	20.0000	-3.2517
25.0000	7.6568	25.0000	-3.4189
30.0000	8.1166	30.0000	-3.5053
35.0000	8.4165	35.0000	-3.5149
40.0000	8.5492	40.0000	-3.4359
45.0000	8.4878	45.0000	-3.2358
50.0000	8.2627	50.0000	-2.9442
55.0000	7.8970	55.0000	-2.5876
60.0000	7.4095	60.0000	-2.1901
65.0000	6.8084	65.0000	-1.7677
70.0000	6.1015	70.0000	-1.3409
75.0000	5.2984	75.0000	-0.9410
80.0000	4.3964	80.0000	-0.6133
85.0000	3.3526	85.0000	-0.4234
90.0000	2.2632	90.0000	-0.2710
95.0000	1.1440	95.0000	-0.1473
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 1.021 percent c
slope of mean line at LE = 0.1902

NACA 64A412
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.3207	1.0554	0.6793	-0.8305
0.5494	1.2977	0.9506	-0.9814
1.0215	1.6865	1.4785	-1.2040
2.2328	2.4214	2.7672	-1.5776
4.6991	3.4923	5.3009	-2.0499
7.1869	4.3214	7.8131	-2.3760
9.6845	5.0173	10.3155	-2.6332
14.6976	6.1304	15.3024	-3.0077
19.7243	6.9837	20.2757	-3.2633
24.7596	7.6305	25.2404	-3.4248
29.8005	8.1014	30.1995	-3.5071
34.8450	8.4096	35.1550	-3.5139
39.8920	8.5484	40.1080	-3.4329
44.9400	8.4896	45.0600	-3.2328
49.9864	8.2635	50.0136	-2.9433
55.0294	7.8945	54.9706	-2.5899
60.0679	7.4020	59.9321	-2.1957
65.1009	6.7952	64.8991	-1.7764
70.1280	6.0821	69.8720	-1.3516
75.1501	5.2730	74.8499	-0.9524
80.1798	4.3611	79.8202	-0.6224
85.1754	3.3147	84.8246	-0.4291
90.1231	2.2361	89.8769	-0.2744
95.0627	1.1297	94.9373	-0.1489
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 1.021 percent c
slope of mean line at LE = 0.1902

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NACA Section 64A612
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	1.4035	0.5000	-0.5977
0.7500	1.6445	0.7500	-0.7475
1.2500	2.0509	1.2500	-0.9570
2.5000	2.8388	2.5000	-1.2738
5.0000	4.0209	5.0000	-1.6245
7.5000	4.9509	7.5000	-1.8391
10.0000	5.7361	10.0000	-1.9961
15.0000	6.9998	15.0000	-2.2012
20.0000	7.9760	20.0000	-2.3175
25.0000	8.7223	25.0000	-2.3657
30.0000	9.2735	30.0000	-2.3566
35.0000	9.6443	35.0000	-2.2919
40.0000	9.8287	40.0000	-2.1588
45.0000	9.8012	45.0000	-1.9233
50.0000	9.5924	50.0000	-1.6146
55.0000	9.2244	55.0000	-1.2604
60.0000	8.7148	60.0000	-0.8858
65.0000	8.0700	65.0000	-0.5090
70.0000	7.2943	70.0000	-0.1535
75.0000	6.3920	75.0000	0.1441
80.0000	5.3501	80.0000	0.3241
85.0000	4.0948	85.0000	0.2990
90.0000	2.7686	90.0000	0.2197
95.0000	1.3972	95.0000	0.0978
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 1.021 percent c
slope of mean line at LE = 0.2852

NACA 64A612
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.2367	1.0917	0.7633	-0.7544
0.4546	1.3559	1.0454	-0.8816
0.9123	1.7856	1.5877	-1.0618
2.1036	2.6107	2.8964	-1.3451
4.5519	3.8329	5.4481	-1.6693
7.0328	4.7897	7.9672	-1.8717
9.5288	5.5973	10.4712	-2.0211
14.5477	6.8987	15.4523	-2.2146
19.5872	7.9046	20.4128	-2.3239
24.6398	8.6754	25.3602	-2.3669
29.7009	9.2457	30.2991	-2.3543
34.7677	9.6310	35.2323	-2.2875
39.8381	9.8261	40.1619	-2.1528
44.9100	9.8034	45.0900	-1.9182
49.9796	9.5936	50.0204	-1.6133
55.0441	9.2205	54.9559	-1.2636
60.1018	8.7030	59.8982	-0.8935
65.1513	8.0484	64.8487	-0.5202
70.1919	7.2620	69.8081	-0.1662
75.2249	6.3487	74.7751	0.1323
80.2688	5.2878	79.7312	0.3203
85.2617	4.0260	84.7383	0.3024
90.1836	2.7191	89.8164	0.2234
95.0935	1.3712	94.9065	0.1001
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 1.021 percent c
slope of mean line at LE = 0.2852

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NACA Section 64A114
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	1.1788	0.5000	-1.0139
0.7500	1.4114	0.7500	-1.2373
1.2500	1.7843	1.2500	-1.5793
2.5000	2.4726	2.5000	-2.1929
5.0000	3.4459	5.0000	-3.0318
7.5000	4.1811	7.5000	-3.6502
10.0000	4.7902	10.0000	-4.1566
15.0000	5.7458	15.0000	-4.9389
20.0000	6.4632	20.0000	-5.5152
25.0000	6.9907	25.0000	-5.9282
30.0000	7.3577	30.0000	-6.2032
35.0000	7.5740	35.0000	-6.3481
40.0000	7.6267	40.0000	-6.3487
45.0000	7.4842	45.0000	-6.1717
50.0000	7.1844	50.0000	-5.8550
55.0000	6.7565	55.0000	-5.4287
60.0000	6.2244	60.0000	-4.9184
65.0000	5.6014	65.0000	-4.3393
70.0000	4.9037	70.0000	-3.7109
75.0000	4.1521	75.0000	-3.0596
80.0000	3.3645	80.0000	-2.4149
85.0000	2.5423	85.0000	-1.8063
90.0000	1.7075	90.0000	-1.2069
95.0000	0.8699	95.0000	-0.6194
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 1.324 percent c
slope of mean line at LE = 0.0475

NACA 64A114
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.4480	1.1220	0.5520	-1.0658
0.6918	1.3613	0.8082	-1.2823
1.1836	1.7395	1.3164	-1.6189
2.4222	2.4356	2.5778	-2.2247
4.9121	3.4168	5.0879	-3.0562
7.4085	4.1567	7.5915	-3.6704
9.9078	4.7696	10.0922	-4.1735
14.9116	5.7313	15.0884	-4.9506
19.9194	6.4532	20.0806	-5.5231
24.9298	6.9844	25.0702	-5.9330
29.9417	7.3542	30.0583	-6.2057
34.9548	7.5727	35.0452	-6.3488
39.9685	7.6270	40.0315	-6.3481
44.9825	7.4850	45.0175	-6.1708
49.9960	7.1847	50.0040	-5.8547
55.0085	6.7556	54.9915	-5.4295
60.0197	6.2222	59.9803	-4.9206
65.0293	5.5975	64.9707	-4.3429
70.0371	4.8983	69.9629	-3.7156
75.0435	4.1454	74.9565	-3.0653
80.0521	3.3561	79.9479	-2.4214
85.0509	2.5338	84.9491	-1.8124
90.0357	1.7016	89.9643	-1.2111
95.0182	0.8668	94.9818	-0.6216
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 1.324 percent c
slope of mean line at LE = 0.0475

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NACA Section 64A215
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	-0.0000	0.0000	0.0000
0.5000	1.3414	0.5000	-0.9871
0.7500	1.5937	0.7500	-1.2205
1.2500	2.0067	1.2500	-1.5737
2.5000	2.7796	2.5000	-2.2002
5.0000	3.8870	5.0000	-3.0428
7.5000	4.7301	7.5000	-3.6551
10.0000	5.4313	10.0000	-4.1526
15.0000	6.5361	15.0000	-4.9143
20.0000	7.3702	20.0000	-5.4689
25.0000	7.9880	25.0000	-5.8598
30.0000	8.4231	30.0000	-6.1125
35.0000	8.6864	35.0000	-6.2341
40.0000	8.7634	40.0000	-6.2077
45.0000	8.6223	45.0000	-5.9979
50.0000	8.3055	50.0000	-5.6467
55.0000	7.8435	55.0000	-5.1874
60.0000	7.2614	60.0000	-4.6481
65.0000	6.5726	65.0000	-4.0462
70.0000	5.7930	70.0000	-3.4045
75.0000	4.9429	75.0000	-2.7543
80.0000	4.0361	80.0000	-2.1328
85.0000	3.0595	85.0000	-1.5834
90.0000	2.0570	90.0000	-1.0531
95.0000	1.0473	95.0000	-0.5449
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 1.481 percent c
slope of mean line at LE = 0.0951

NACA 64A215
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.3903	1.2096	0.6097	-1.0972
0.6271	1.4752	0.8729	-1.3171
1.1094	1.8995	1.3906	-1.6582
2.3344	2.6899	2.6656	-2.2681
4.8124	3.8156	5.1876	-3.0944
7.3044	4.6701	7.6956	-3.6974
9.8027	5.3801	10.1973	-4.1881
14.8108	6.4999	15.1892	-4.9385
19.8274	7.3452	20.1726	-5.4850
24.8495	7.9721	25.1505	-5.8693
29.8751	8.4143	30.1249	-6.1171
34.9031	8.6830	35.0969	-6.2351
39.9325	8.7638	40.0675	-6.2061
44.9626	8.6241	45.0374	-5.9957
49.9915	8.3061	50.0085	-5.6460
55.0183	7.8415	54.9817	-5.1892
60.0421	7.2561	59.9579	-4.6529
65.0625	6.5634	64.9375	-4.0540
70.0792	5.7801	69.9208	-3.4148
75.0928	4.9266	74.9072	-2.7663
80.1111	4.0151	79.8889	-2.1457
85.1086	3.0378	84.8915	-1.5950
90.0761	2.0418	89.9239	-1.0609
95.0389	1.0393	94.9611	-0.5489
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 1.481 percent c
slope of mean line at LE = 0.0951

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NACA Section 64A415
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	-0.0000	0.0000	0.0000
0.5000	1.5303	0.5000	-0.8348
0.7500	1.7960	0.7500	-1.0520
1.2500	2.2391	1.2500	-1.3756
2.5000	3.0847	2.5000	-1.9272
5.0000	4.3230	5.0000	-2.6355
7.5000	5.2803	7.5000	-3.1307
10.0000	6.0816	10.0000	-3.5248
15.0000	7.3556	15.0000	-4.1122
20.0000	8.3271	20.0000	-4.5247
25.0000	9.0565	25.0000	-4.8003
30.0000	9.5813	30.0000	-4.9602
35.0000	9.9143	35.0000	-5.0098
40.0000	10.0421	40.0000	-4.9307
45.0000	9.9348	45.0000	-4.6860
50.0000	9.6348	50.0000	-4.3174
55.0000	9.1715	55.0000	-3.8594
60.0000	8.5685	60.0000	-3.3418
65.0000	7.8368	65.0000	-2.7840
70.0000	6.9892	70.0000	-2.2122
75.0000	6.0402	75.0000	-1.6631
80.0000	4.9936	80.0000	-1.1873
85.0000	3.8049	85.0000	-0.8528
90.0000	2.5645	90.0000	-0.5566
95.0000	1.3015	95.0000	-0.2967
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 1.481 percent c
slope of mean line at LE = 0.1902

NACA 64A415
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.2836	1.2507	0.7164	-1.0258
0.5071	1.5384	0.9929	-1.2222
0.9713	2.0038	1.5287	-1.5213
2.1710	2.8845	2.8290	-2.0408
4.6264	4.1611	5.3736	-2.7187
7.1100	5.1428	7.8900	-3.1974
9.6064	5.9640	10.3936	-3.5799
14.6221	7.2712	15.3779	-4.1484
19.6552	8.2684	20.3448	-4.5479
24.6992	9.0187	25.3008	-4.8130
29.7503	9.5596	30.2497	-4.9654
34.8062	9.9050	35.1938	-5.0093
39.8651	10.0418	40.1349	-4.9263
44.9252	9.9380	45.0748	-4.6812
49.9830	9.6362	50.0170	-4.3159
55.0366	9.1676	54.9634	-3.8630
60.0842	8.5572	59.9158	-3.3509
65.1250	7.8170	64.8750	-2.7982
70.1582	6.9606	69.8418	-2.2301
75.1854	6.0034	74.8146	-1.6828
80.2218	4.9438	79.7782	-1.2051
85.2164	3.7516	84.7836	-0.8660
90.1516	2.5266	89.8484	-0.5649
95.0776	1.2817	94.9224	-0.3008
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 1.481 percent c
slope of mean line at LE = 0.1902

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NACA Section 64A218
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	1.5557	0.5000	-1.1205
0.7500	1.8496	0.7500	-1.3973
1.2500	2.3367	1.2500	-1.8268
2.5000	3.2550	2.5000	-2.6069
5.0000	4.5689	5.0000	-3.6697
7.5000	5.5650	7.5000	-4.4437
10.0000	6.3912	10.0000	-5.0734
15.0000	7.6886	15.0000	-6.0394
20.0000	8.6646	20.0000	-6.7448
25.0000	9.3840	25.0000	-7.2444
30.0000	9.8869	30.0000	-7.5704
35.0000	10.1843	35.0000	-7.7303
40.0000	10.2542	40.0000	-7.6998
45.0000	10.0633	45.0000	-7.4408
50.0000	9.6675	50.0000	-7.0094
55.0000	9.1044	55.0000	-6.4466
60.0000	8.4030	60.0000	-5.7851
65.0000	7.5818	65.0000	-5.0480
70.0000	6.6596	70.0000	-4.2612
75.0000	5.6648	75.0000	-3.4645
80.0000	4.6143	80.0000	-2.6972
85.0000	3.4960	85.0000	-2.0063
90.0000	2.3461	90.0000	-1.3329
95.0000	1.2006	95.0000	-0.6935
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 1.945 percent c
slope of mean line at LE = 0.0951

NACA 64A218
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.3741	1.3807	0.6259	-1.2682
0.6083	1.6888	0.8917	-1.5307
1.0865	2.1886	1.4135	-1.9474
2.3050	3.1290	2.6950	-2.7071
4.7770	4.4682	5.2230	-3.7470
7.2665	5.4802	7.7335	-4.5076
9.7640	6.3191	10.2360	-5.1270
14.7731	7.6376	15.2269	-6.0762
19.7929	8.6296	20.2071	-6.7694
24.8193	9.3619	25.1807	-7.2591
29.8500	9.8748	30.1500	-7.5776
34.8836	10.1798	35.1164	-7.7320
39.9191	10.2552	40.0809	-7.6974
44.9552	10.0660	45.0448	-7.4376
49.9899	9.6685	50.0101	-7.0084
55.0218	9.1016	54.9782	-6.4493
60.0502	8.3953	59.9498	-5.7922
65.0743	7.5688	64.9257	-5.0594
70.0940	6.6415	69.9060	-4.2762
75.1100	5.6423	74.8900	-3.4820
80.1317	4.5857	79.8683	-2.7163
85.1286	3.4665	84.8714	-2.0238
90.0900	2.3255	89.9100	-1.3447
95.0463	1.1899	94.9537	-0.6995
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 1.945 percent c
slope of mean line at LE = 0.0951

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NACA Section 64A221
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	-0.0000	0.0000	0.0000
0.5000	1.7387	0.5000	-1.2256
0.7500	2.0719	0.7500	-1.5396
1.2500	2.6323	1.2500	-2.0391
2.5000	3.7014	2.5000	-2.9736
5.0000	5.2313	5.0000	-4.2664
7.5000	6.3859	7.5000	-5.2095
10.0000	7.3412	10.0000	-5.9765
15.0000	8.8364	15.0000	-7.1543
20.0000	9.9578	20.0000	-8.0156
25.0000	10.7809	25.0000	-8.6276
30.0000	11.3524	30.0000	-9.0288
35.0000	11.6831	35.0000	-9.2273
40.0000	11.7431	40.0000	-9.1905
45.0000	11.4983	45.0000	-8.8783
50.0000	11.0201	50.0000	-8.3628
55.0000	10.3532	55.0000	-7.6934
60.0000	9.5307	60.0000	-6.9074
65.0000	8.5745	65.0000	-6.0320
70.0000	7.5113	70.0000	-5.1016
75.0000	6.3741	75.0000	-4.1604
80.0000	5.1819	80.0000	-3.2490
85.0000	3.9244	85.0000	-2.4191
90.0000	2.6289	90.0000	-1.6053
95.0000	1.3530	95.0000	-0.8404
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 2.366 percent c
slope of mean line at LE = 0.0951

NACA 64A221
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.3607	1.5214	0.6393	-1.4090
0.5926	1.8677	0.9074	-1.7096
1.0666	2.4398	1.4334	-2.1986
2.2780	3.5336	2.7220	-3.1117
4.7429	5.0962	5.2571	-4.3750
7.2295	6.2721	7.7705	-5.2994
9.7258	7.2444	10.2742	-6.0524
14.7357	8.7680	15.2643	-7.2066
19.7584	9.9109	20.2416	-8.0506
24.7891	10.7514	25.2109	-8.6486
29.8249	11.3364	30.1751	-9.0393
34.8641	11.6775	35.1359	-9.2297
39.9057	11.7448	40.0943	-9.1871
44.9478	11.5022	45.0522	-8.8738
49.9882	11.0215	50.0118	-8.3614
55.0253	10.3494	54.9747	-7.6971
60.0581	9.5203	59.9419	-6.9171
65.0860	8.5570	64.9140	-6.0477
70.1086	7.4873	69.8914	-5.1220
75.1270	6.3445	74.8730	-4.1842
80.1518	5.1447	79.8482	-3.2754
85.1483	3.8862	84.8517	-2.4434
90.1036	2.6023	89.8964	-1.6215
95.0536	1.3391	94.9464	-0.8487
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 2.366 percent c
slope of mean line at LE = 0.0951

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NACA Section 65A210
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	0.8899	0.5000	-0.6677
0.7500	1.0671	0.7500	-0.8139
1.2500	1.3591	1.2500	-1.0328
2.5000	1.8751	2.5000	-1.3924
5.0000	2.5741	5.0000	-1.8069
7.5000	3.1630	7.5000	-2.1476
10.0000	3.6594	10.0000	-2.4315
15.0000	4.4563	15.0000	-2.8690
20.0000	5.0694	20.0000	-3.1911
25.0000	5.5418	25.0000	-3.4271
30.0000	5.8940	30.0000	-3.5899
35.0000	6.1374	35.0000	-3.6863
40.0000	6.2732	40.0000	-3.7148
45.0000	6.2956	45.0000	-3.6678
50.0000	6.1917	50.0000	-3.5320
55.0000	5.9575	55.0000	-3.3037
60.0000	5.6049	60.0000	-2.9972
65.0000	5.1556	65.0000	-2.6382
70.0000	4.6187	70.0000	-2.2418
75.0000	3.9989	75.0000	-1.8234
80.0000	3.2977	80.0000	-1.4089
85.0000	2.5043	85.0000	-1.0422
90.0000	1.6879	90.0000	-0.6935
95.0000	0.8528	95.0000	-0.3553
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 0.654 percent c
slope of mean line at LE = 0.0951

NACA 65A210
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.4266	0.8280	0.5734	-0.7156
0.6679	1.0122	0.8321	-0.8541
1.1560	1.3093	1.3440	-1.0680
2.3913	1.8376	2.6087	-1.4158
4.8814	2.5446	5.1186	-1.8234
7.3761	3.1360	7.6239	-2.1633
9.8746	3.6364	10.1254	-2.4443
14.8789	4.4394	15.1211	-2.8780
19.8890	5.0575	20.1110	-3.1972
24.9025	5.5338	25.0975	-3.4309
29.9185	5.8892	30.0815	-3.5920
34.9362	6.1349	35.0638	-3.6871
39.9550	6.2725	40.0450	-3.7147
44.9745	6.2958	45.0255	-3.6674
49.9941	6.1919	50.0059	-3.5318
55.0130	5.9567	54.9870	-3.3044
60.0304	5.6024	59.9696	-2.9993
65.0459	5.1510	64.9541	-2.6416
70.0590	4.6119	69.9410	-2.2466
75.0702	3.9897	74.9298	-1.8294
80.0848	3.2849	79.9152	-1.4156
85.0829	2.4908	84.9171	-1.0480
90.0583	1.6783	89.9417	-0.6974
95.0295	0.8478	94.9704	-0.3573
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 0.654 percent c
slope of mean line at LE = 0.0951

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NACA Section 65A112
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	-0.0000	0.0000	0.0000
0.5000	1.0487	0.5000	-0.7839
0.7500	1.2565	0.7500	-0.9631
1.2500	1.5988	1.2500	-1.2363
2.5000	2.2002	2.5000	-1.6907
5.0000	3.0112	5.0000	-2.2236
7.5000	3.6960	7.5000	-2.6616
10.0000	4.2713	10.0000	-3.0276
15.0000	5.1928	15.0000	-3.5940
20.0000	5.8999	20.0000	-4.0135
25.0000	6.4431	25.0000	-4.3231
30.0000	6.8464	30.0000	-4.5393
35.0000	7.1228	35.0000	-4.6703
40.0000	7.2732	40.0000	-4.7146
45.0000	7.2896	45.0000	-4.6622
50.0000	7.1561	50.0000	-4.4966
55.0000	6.8693	55.0000	-4.2149
60.0000	6.4461	60.0000	-3.8364
65.0000	5.9126	65.0000	-3.3916
70.0000	5.2805	70.0000	-2.8984
75.0000	4.5569	75.0000	-2.3749
80.0000	3.7462	80.0000	-1.8493
85.0000	2.8416	85.0000	-1.3714
90.0000	1.9127	90.0000	-0.9127
95.0000	0.9684	95.0000	-0.4681
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 0.891 percent c
slope of mean line at LE = 0.0951

NACA 65A112
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.4137	0.9641	0.5863	-0.8517
0.6531	1.1800	0.8469	-1.0219
1.1386	1.5295	1.3614	-1.2883
2.3706	2.1481	2.6294	-1.7262
4.8583	2.9702	5.1417	-2.2490
7.3517	3.6583	7.6483	-2.6857
9.8498	4.2394	10.1502	-3.0473
14.8548	5.1694	15.1452	-3.6080
19.8667	5.8833	20.1333	-4.0231
24.8830	6.4320	25.1170	-4.3292
29.9022	6.8398	30.0978	-4.5426
34.9234	7.1195	35.0766	-4.6717
39.9460	7.2723	40.0540	-4.7146
44.9694	7.2899	45.0306	-4.6616
49.9929	7.1564	50.0071	-4.4963
55.0156	6.8682	54.9845	-4.2159
60.0364	6.4426	59.9636	-3.8394
65.0548	5.9062	64.9452	-3.3968
70.0704	5.2709	69.9296	-2.9056
75.0835	4.5441	74.9165	-2.3838
80.1008	3.7288	79.8992	-1.8594
85.0985	2.8233	84.9015	-1.3805
90.0691	1.8997	89.9309	-0.9189
95.0351	0.9617	94.9649	-0.4713
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 0.891 percent c
slope of mean line at LE = 0.0951

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NACA Section 65A212
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	-0.0000	0.0000	0.0000
0.5000	1.0487	0.5000	-0.7839
0.7500	1.2565	0.7500	-0.9631
1.2500	1.5988	1.2500	-1.2363
2.5000	2.2002	2.5000	-1.6907
5.0000	3.0112	5.0000	-2.2236
7.5000	3.6960	7.5000	-2.6616
10.0000	4.2713	10.0000	-3.0276
15.0000	5.1928	15.0000	-3.5940
20.0000	5.8999	20.0000	-4.0135
25.0000	6.4431	25.0000	-4.3231
30.0000	6.8464	30.0000	-4.5393
35.0000	7.1228	35.0000	-4.6703
40.0000	7.2732	40.0000	-4.7146
45.0000	7.2896	45.0000	-4.6622
50.0000	7.1561	50.0000	-4.4966
55.0000	6.8693	55.0000	-4.2149
60.0000	6.4461	60.0000	-3.8364
65.0000	5.9126	65.0000	-3.3916
70.0000	5.2805	70.0000	-2.8984
75.0000	4.5569	75.0000	-2.3749
80.0000	3.7462	80.0000	-1.8493
85.0000	2.8416	85.0000	-1.3714
90.0000	1.9127	90.0000	-0.9127
95.0000	0.9684	95.0000	-0.4681
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 0.891 percent c
slope of mean line at LE = 0.0951

NACA 65A212
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.4137	0.9641	0.5863	-0.8517
0.6531	1.1800	0.8469	-1.0219
1.1386	1.5295	1.3614	-1.2883
2.3706	2.1481	2.6294	-1.7262
4.8583	2.9702	5.1417	-2.2490
7.3517	3.6583	7.6483	-2.6857
9.8498	4.2394	10.1502	-3.0473
14.8548	5.1694	15.1452	-3.6080
19.8667	5.8833	20.1333	-4.0231
24.8830	6.4320	25.1170	-4.3292
29.9022	6.8398	30.0978	-4.5426
34.9234	7.1195	35.0766	-4.6717
39.9460	7.2723	40.0540	-4.7146
44.9694	7.2899	45.0306	-4.6616
49.9929	7.1564	50.0071	-4.4963
55.0156	6.8682	54.9845	-4.2159
60.0364	6.4426	59.9636	-3.8394
65.0548	5.9062	64.9452	-3.3968
70.0704	5.2709	69.9296	-2.9056
75.0835	4.5441	74.9165	-2.3838
80.1008	3.7288	79.8992	-1.8594
85.0985	2.8233	84.9015	-1.3805
90.0691	1.8997	89.9309	-0.9189
95.0351	0.9617	94.9649	-0.4713
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 0.891 percent c
slope of mean line at LE = 0.0951

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NACA Section 65A412
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	1.1912	0.5000	-0.6685
0.7500	1.4165	0.7500	-0.8304
1.2500	1.7919	1.2500	-1.0688
2.5000	2.4664	2.5000	-1.4481
5.0000	3.4165	5.0000	-1.8417
7.5000	4.2230	7.5000	-2.1544
10.0000	4.9020	10.0000	-2.4148
15.0000	5.9990	15.0000	-2.8016
20.0000	6.8481	20.0000	-3.0755
25.0000	7.5066	25.0000	-3.2668
30.0000	8.0024	30.0000	-3.3881
35.0000	8.3505	35.0000	-3.4455
40.0000	8.5533	40.0000	-3.4360
45.0000	8.6035	45.0000	-3.3488
50.0000	8.4859	50.0000	-3.1669
55.0000	8.1966	55.0000	-2.8877
60.0000	7.7513	60.0000	-2.5319
65.0000	7.1739	65.0000	-2.1320
70.0000	6.4732	70.0000	-1.7092
75.0000	5.6507	75.0000	-1.2867
80.0000	4.7000	80.0000	-0.9064
85.0000	3.5834	85.0000	-0.6430
90.0000	2.4176	90.0000	-0.4177
95.0000	1.2213	95.0000	-0.2207
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 0.891 percent c
slope of mean line at LE = 0.1902

NACA 65A412
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.3296	1.0084	0.6704	-0.7835
0.5584	1.2466	0.9416	-0.9304
1.0293	1.6372	1.4707	-1.1547
2.2429	2.3463	2.7571	-1.5025
4.7178	3.3194	5.2822	-1.8770
7.2043	4.1343	7.7957	-2.1890
9.7003	4.8262	10.2997	-2.4421
14.7100	5.9429	15.2900	-2.8201
19.7338	6.8081	20.2662	-3.0876
24.7662	7.4796	25.2338	-3.2739
29.8044	7.9858	30.1956	-3.3915
34.8468	8.3419	35.1532	-3.4463
39.8920	8.5505	40.1080	-3.4350
44.9388	8.6039	45.0612	-3.3471
49.9858	8.4865	50.0142	-3.1662
55.0311	8.1943	54.9689	-2.8897
60.0727	7.7438	59.9273	-2.5375
65.1095	7.1599	64.8905	-2.1411
70.1407	6.4517	69.8593	-1.7212
75.1669	5.6213	74.8331	-1.3006
80.2012	4.6580	79.7988	-0.9193
85.1963	3.5379	84.8037	-0.6523
90.1377	2.3851	89.8623	-0.4234
95.0700	1.2043	94.9300	-0.2235
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 0.891 percent c
slope of mean line at LE = 0.1902

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NACA Section 65A215
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	1.2721	0.5000	-0.9359
0.7500	1.5256	0.7500	-1.1621
1.2500	1.9446	1.2500	-1.5169
2.5000	2.6759	2.5000	-2.1176
5.0000	3.6575	5.0000	-2.8323
7.5000	4.4890	7.5000	-3.4192
10.0000	5.1847	10.0000	-3.9114
15.0000	6.2955	15.0000	-4.6753
20.0000	7.1450	20.0000	-5.2436
25.0000	7.7954	25.0000	-5.6656
30.0000	8.2759	30.0000	-5.9630
35.0000	8.6019	35.0000	-6.1469
40.0000	8.7737	40.0000	-6.2146
45.0000	8.7789	45.0000	-6.1522
50.0000	8.5982	50.0000	-5.9391
55.0000	8.2288	55.0000	-5.5730
60.0000	7.6966	60.0000	-5.0832
65.0000	7.0352	65.0000	-4.5078
70.0000	6.2594	70.0000	-3.8681
75.0000	5.3799	75.0000	-3.1860
80.0000	4.4057	80.0000	-2.4942
85.0000	3.3370	85.0000	-1.8525
90.0000	2.2422	90.0000	-1.2324
95.0000	1.1392	95.0000	-0.6339
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 1.251 percent c
slope of mean line at LE = 0.0951

NACA 65A215
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.3961	1.1492	0.6039	-1.0367
0.6327	1.4114	0.8673	-1.2533
1.1140	1.8408	1.3860	-1.5996
2.3405	2.5977	2.6595	-2.1758
4.8243	3.5958	5.1757	-2.8746
7.3155	4.4321	7.6845	-3.4594
9.8128	5.1366	10.1872	-3.9445
14.8187	6.2603	15.1813	-4.6989
19.8335	7.1201	20.1665	-5.2599
24.8537	7.7789	25.1463	-5.6760
29.8777	8.2660	30.1223	-5.9689
34.9042	8.5971	35.0958	-6.1493
39.9325	8.7724	40.0675	-6.2147
44.9618	8.7796	45.0382	-6.1512
49.9912	8.5987	50.0088	-5.9386
55.0194	8.2270	54.9806	-5.5747
60.0452	7.6912	59.9548	-5.0880
65.0679	7.0254	64.9321	-4.5161
70.0872	6.2449	69.9128	-3.8797
75.1032	5.3608	74.8968	-3.2005
80.1243	4.3802	79.8757	-2.5108
85.1213	3.3105	84.8787	-1.8677
90.0850	2.2235	89.9150	-1.2427
95.0434	1.1295	94.9566	-0.6391
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 1.251 percent c
slope of mean line at LE = 0.0951

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NACA Section 65A415
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	1.4544	0.5000	-0.7925
0.7500	1.7253	0.7500	-1.0001
1.2500	2.1723	1.2500	-1.3205
2.5000	2.9684	2.5000	-1.8529
5.0000	4.0846	5.0000	-2.4347
7.5000	5.0356	7.5000	-2.8967
10.0000	5.8320	10.0000	-3.2859
15.0000	7.1138	15.0000	-3.8737
20.0000	8.1018	20.0000	-4.2993
25.0000	8.8646	25.0000	-4.6052
30.0000	9.4352	30.0000	-4.8096
35.0000	9.8312	35.0000	-4.9211
40.0000	10.0541	40.0000	-4.9359
45.0000	10.0925	45.0000	-4.8392
50.0000	9.9278	50.0000	-4.6096
55.0000	9.5567	55.0000	-4.2452
60.0000	9.0037	60.0000	-3.7768
65.0000	8.3000	65.0000	-3.2451
70.0000	7.4572	70.0000	-2.6746
75.0000	6.4802	75.0000	-2.0925
80.0000	5.3680	80.0000	-1.5452
85.0000	4.0876	85.0000	-1.1186
90.0000	2.7533	90.0000	-0.7338
95.0000	1.3954	95.0000	-0.3847
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 1.251 percent c
slope of mean line at LE = 0.1902

NACA 65A415
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.2949	1.1910	0.7051	-0.9661
0.5182	1.4753	0.9818	-1.1591
0.9805	1.9457	1.5195	-1.4631
2.1832	2.7929	2.8168	-1.9491
4.6502	3.9422	5.3498	-2.4998
7.1322	4.9056	7.8678	-2.9602
9.6265	5.7211	10.3735	-3.3370
14.6380	7.0320	15.3620	-3.9093
19.6673	8.0435	20.3327	-4.3231
24.7076	8.8255	25.2924	-4.6199
29.7554	9.4114	30.2446	-4.8171
34.8084	9.8192	35.1916	-4.9235
39.8649	10.0504	40.1351	-4.9349
44.9236	10.0934	45.0764	-4.8367
49.9823	9.9287	50.0177	-4.6085
55.0387	9.5531	54.9613	-4.2485
60.0904	8.9923	59.9096	-3.7860
65.1358	8.2789	64.8642	-3.2602
70.1743	7.4253	69.8257	-2.6948
75.2063	6.4372	74.7937	-2.1166
80.2481	5.3081	79.7519	-1.5694
85.2419	4.0235	84.7581	-1.1379
90.1694	2.7077	89.8306	-0.7461
95.0864	1.3716	94.9136	-0.3908
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 1.251 percent c
slope of mean line at LE = 0.1902

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NACA Section 65A615
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	1.6462	0.5000	-0.6700
0.7500	1.9345	0.7500	-0.8539
1.2500	2.4072	1.2500	-1.1377
2.5000	3.2689	2.5000	-1.5985
5.0000	4.5207	5.0000	-2.0472
7.5000	5.5897	7.5000	-2.3829
10.0000	6.4861	10.0000	-2.6679
15.0000	7.9374	15.0000	-3.0779
20.0000	9.0625	20.0000	-3.3592
25.0000	9.9367	25.0000	-3.5479
30.0000	10.5964	30.0000	-3.6581
35.0000	11.0615	35.0000	-3.6965
40.0000	11.3350	40.0000	-3.6579
45.0000	11.4064	45.0000	-3.5263
50.0000	11.2573	50.0000	-3.2801
55.0000	10.8847	55.0000	-2.9174
60.0000	10.3111	60.0000	-2.4708
65.0000	9.5655	65.0000	-1.9831
70.0000	8.6563	70.0000	-1.4826
75.0000	7.5826	75.0000	-1.0014
80.0000	6.3343	80.0000	-0.6011
85.0000	4.8437	85.0000	-0.3902
90.0000	3.2685	90.0000	-0.2393
95.0000	1.6538	95.0000	-0.1377
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 1.251 percent c
slope of mean line at LE = 0.2852

NACA 65A615
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.1989	1.2244	0.8011	-0.8871
0.4086	1.5303	1.0914	-1.0560
0.8518	2.0409	1.6482	-1.3171
2.0299	2.9783	2.9701	-1.7126
4.4791	4.2796	5.5209	-2.1160
6.9513	5.3708	8.0487	-2.4528
9.4421	6.2981	10.5579	-2.7219
14.4584	7.7979	15.5416	-3.1137
19.5018	8.9625	20.4982	-3.3818
24.5619	9.8690	25.4381	-3.5605
29.6334	10.5547	30.3666	-3.6633
34.7127	11.0400	35.2873	-3.6965
39.7975	11.3277	40.2025	-3.6545
44.8854	11.4071	45.1146	-3.5220
49.9735	11.2587	50.0265	-3.2784
55.0581	10.8791	54.9419	-2.9222
60.1356	10.2931	59.8644	-2.4836
65.2037	9.5316	64.7963	-2.0035
70.2612	8.6042	69.7388	-1.5084
75.3090	7.5112	74.6910	-1.0302
80.3709	6.2317	79.6291	-0.6237
85.3608	4.7309	84.6392	-0.4025
90.2526	3.1880	89.7474	-0.2454
95.1289	1.6116	94.8711	-0.1403
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 1.251 percent c
slope of mean line at LE = 0.2852

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NACA Section 65A418
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	1.6981	0.5000	-0.8889
0.7500	2.0154	0.7500	-1.1361
1.2500	2.5356	1.2500	-1.5333
2.5000	3.4559	2.5000	-2.2231
5.0000	4.7414	5.0000	-2.9999
7.5000	5.8406	7.5000	-3.6152
10.0000	6.7570	10.0000	-4.1380
15.0000	8.2265	15.0000	-4.9337
20.0000	9.3550	20.0000	-5.5155
25.0000	10.2232	25.0000	-5.9397
30.0000	10.8691	30.0000	-6.2294
35.0000	11.3130	35.0000	-6.3965
40.0000	11.5551	40.0000	-6.4361
45.0000	11.5795	45.0000	-6.3280
50.0000	11.3641	50.0000	-6.0469
55.0000	10.9077	55.0000	-5.5929
60.0000	10.2437	60.0000	-5.0075
65.0000	9.4121	65.0000	-4.3412
70.0000	8.4255	70.0000	-3.6204
75.0000	7.2937	75.0000	-2.8777
80.0000	6.0225	80.0000	-2.1654
85.0000	4.5821	85.0000	-1.5791
90.0000	3.0810	90.0000	-1.0386
95.0000	1.5673	95.0000	-0.5448
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 1.594 percent c
slope of mean line at LE = 0.1902

NACA 65A418
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.2652	1.3473	0.7348	-1.1224
0.4830	1.6750	1.0170	-1.3588
0.9362	2.2258	1.5638	-1.7433
2.1267	3.2159	2.8733	-2.3721
4.5847	4.5456	5.4153	-3.1031
7.0616	5.6614	7.9385	-3.7161
9.5536	6.6043	10.4464	-4.2202
14.5663	8.1142	15.4337	-4.9914
19.6010	9.2752	20.3990	-5.5547
24.6492	10.1699	25.3508	-5.9642
29.7064	10.8368	30.2936	-6.2426
34.7700	11.2969	35.2300	-6.4012
39.8379	11.5506	40.1621	-6.4350
44.9083	11.5812	45.0917	-6.3244
49.9788	11.3655	50.0212	-6.0453
55.0463	10.9024	54.9537	-5.5978
60.1079	10.2274	59.8921	-5.0211
65.1618	9.3825	64.8382	-4.3638
70.2072	8.3814	69.7928	-3.6509
75.2448	7.2350	74.7552	-2.9143
80.2938	5.9423	79.7062	-2.2036
85.2862	4.4967	84.7138	-1.6111
90.2001	3.0207	89.7999	-1.0590
95.1025	1.5359	94.8975	-0.5550
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 1.594 percent c
slope of mean line at LE = 0.1902

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NACA Section 65A421
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.5000	1.9130	0.5000	-0.9607
0.7500	2.2776	0.7500	-1.2402
1.2500	2.8733	1.2500	-1.7049
2.5000	3.9229	2.5000	-2.5538
5.0000	5.3821	5.0000	-3.5328
7.5000	6.6337	7.5000	-4.3054
10.0000	7.6738	10.0000	-4.9675
15.0000	9.3348	15.0000	-5.9789
20.0000	10.6062	20.0000	-6.7224
25.0000	11.5814	25.0000	-7.2688
30.0000	12.3034	30.0000	-7.6469
35.0000	12.7955	35.0000	-7.8715
40.0000	13.0563	40.0000	-7.9364
45.0000	13.0646	45.0000	-7.8154
50.0000	12.7943	50.0000	-7.4784
55.0000	12.2497	55.0000	-6.9311
60.0000	11.4730	60.0000	-6.2256
65.0000	10.5108	65.0000	-5.4210
70.0000	9.3799	70.0000	-4.5483
75.0000	8.0936	75.0000	-3.6447
80.0000	6.6658	80.0000	-2.7692
85.0000	5.0682	85.0000	-2.0263
90.0000	3.4015	90.0000	-1.3332
95.0000	1.7377	95.0000	-0.7018
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 1.881 percent c
slope of mean line at LE = 0.1902

NACA 65A421
(Stations and ordinates given in per cent of airfoil chord)
Upper Surface		Lower Surface
Station	Ordinate	Station	Ordinate
0.0000	0.0000	0.0000	0.0000
0.2410	1.4742	0.7590	-1.2493
0.4538	1.8409	1.0462	-1.5247
0.8974	2.4710	1.6026	-1.9884
2.0741	3.6096	2.9259	-2.7659
4.5218	5.1246	5.4782	-3.6822
6.9927	6.3975	8.0073	-4.4522
9.4820	7.4725	10.5180	-5.0883
14.4953	9.1871	15.5047	-6.0643
19.5350	10.5014	20.4650	-6.7809
24.5908	11.5115	25.4092	-7.3058
29.6574	12.2614	30.3426	-7.6671
34.7316	12.7749	35.2684	-7.8792
39.8109	13.0509	40.1891	-7.9354
44.8931	13.0673	45.1069	-7.8106
49.9754	12.7964	50.0246	-7.4762
55.0538	12.2425	54.9462	-6.9379
60.1252	11.4510	59.8748	-6.2447
65.1875	10.4714	64.8125	-5.4526
70.2396	9.3216	69.7604	-4.5911
75.2825	8.0169	74.7175	-3.6962
80.3386	6.5627	79.6614	-2.8240
85.3295	4.9590	84.6705	-2.0734
90.2299	3.3250	89.7701	-1.3634
95.1184	1.6978	94.8816	-0.7170
100.0000	-0.0000	100.0000	0.0000
L.E. radius = 1.881 percent c
slope of mean line at LE = 0.1902

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